gsde

高品質積分 Runge Kutta 如有需要仍有更精細版本可供參考(Runge Kutta)

单天线波束形成算法 matlab代码 需要的下(Single-antenna beamforming algorithm matlab code required under)

it is a camera for matlab

可以用此程序进行电动汽车接入配电网的蒙特卡洛模拟(Monte Carlo simulation for electric vehicle to distribution network)

几本粒子群程序。用MATLAB编写。可以更改成自己能用的程序。(Particle Swarm several procedures. Prepared using MATLAB. Can be used to change into their own procedures.)

说明：  UMTS无线网络规划与优化，英文版，本书还附有静态系统级仿真的matlab程序，功能很强大，网上可以下载到 John.Wiley.and.Sons.Radio.Network.Planning.and.Optimisation.for.UMTS.2nd.Edition.pdf(John.Wiley.and.Sons.Radio.Network.Planning.and.Optimisation.for.UMTS.2nd.Edition.pdf)

说明：  用于单轨道金融资产蒙特卡洛模拟的资产价格路径的刻画，实用极强，作为基础函数，方便调用。(Financial assets for single track MC simulations describe the path of asset prices, extremely practical, as the basis functions, easy call.)

关于PNG文件格式的分析,不是很详细,但是中文版的..如果要更好的,请找英文版式(on PNG file format, is not very detailed, but the Chinese version of .. if better, Please find English-)

通过自适应算法来预测将来的变化。是通过matlab来实现的。已经调试完成(Through the adaptive algorithm to predict the future changes. Are achieved through matlab. Have been debug finish)

说明：  月球软着陆仿真：在停泊轨道上，探测器在脉冲制动的作用下，经霍曼变轨，下降到距月面大约 15 公里的近月点，该近月点就是主制动段的初始制动点。主制动段以下是障碍检测与规避和最终着陆段。在主制动段，由于探测器的初始速度很大(1.692km/s)，所以主制动段制导律设计的主要目的就是高效抵消此速度，将探测器导引到期望的末端状态(Lunar soft landing simulation: in the parking orbit, the probe under the action of pulse braking, through the hohmann change of orbit, to descend to about 15 kilometers from the surface of the moon, the near-moon point is the main braking section of the initial braking point. Following is the main braking section for obstacle detection and avoidance and the final landing section. In the main braking section, since the initial velocity of the detector is very large (1.692km/s), the main purpose of the guidance law design of the main braking section is to effectively offset this velocity and guide the detector to the desired terminal state)